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ENDUROSAT'S CUBESAT NANO-SATELLITE AND MODULES SPACE QUALIFICATION TEST CAMPAIGN

机译:ENDUROSAT的CUBESAT纳米卫星和模块空间鉴定测试活动

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There is an increasing demand of nano-satellite development among universities, small companies and emerging countries. Low-cost and fast-delivery are the main advantages of such class of satellites achieved by the extensive use of commercial-off-the-shelf components. On the other side the loss of reliability and the poor success rate are limiting the use of nano-satellite to educational and technology demonstration and not to commercial purpose. Standardization of nano-satellite environmental testing by tailoring the existing test standard for medium/large satellites is then a crucial step for their market growth. Thus it is fundamental to find the right trade-off between the improving of reliability and the need to keep their low-cost/fast-delivery advantages. This is particularly even more essential for satellites of CubeSat family. Such miniaturized and standardized satellites have 10 cm cubic form and mass no more than 1.33 kilograms per 1 unit (1U). For this class of nano-satellites the qualification process is mandatory to reduce the risk of failure during a space mission. This paper reports description and results of the space qualification test campaign performed on Endurosat's Cubesat nano-satellite and modules. Physical properties evaluation (weight, center of gravity and momentum of inertia), thermal cycling, thermal vacuum cycling, vibration (sinusoidal and random) and pyroshock tests have been executed by CIRA's Space Qualification Lab from 3rd to 14th, December 2015. Mechanical and environmental tests have been carried out step by step: from the testing of the single subsystem up to the assembled Cubesat nano-satellite. Functional tests have been performed during all the test campaign to verify the functionalities of the systems. The sequence of the tests followed the "test as you flight" philosophy while durations and levels have been selected by tailoring the ESA standard ECSS-E-ST-10-03C and GEVS GSFC-STD-7000A.
机译:在大学,小型公司和新兴国家中,对纳米卫星开发的需求不断增长。低成本和快速交付是此类卫星的主要优势,这是通过广泛使用现成的商用组件来实现的。另一方面,可靠性的丧失和成功率的下降限制了纳米卫星的使用,仅用于教育和技术演示,而不能用于商业目的。通过为中/大型卫星量身定制现有的测试标准,纳米卫星环境测试的标准化是其市场增长的关键一步。因此,至关重要的是在可靠性的提高与保持其低成本/快速交付优势之间的需要之间找到适当的权衡。对于CubeSat系列卫星来说,这一点尤为重要。这种小型化和标准化的卫星具有10厘米立方的形状,质量不超过每1个单位(1U)1.33千克。对于此类纳米卫星,必须执行鉴定程序,以减少太空飞行任务中发生故障的风险。本文报告了对Endurosat的Cubesat纳米卫星和模块进行的太空资格测试活动的描述和结果。 CIRA的太空鉴定实验室已于2015年12月3日至14日进行了物理性能评估(重量,重心和惯性动量),热循环,热真空循环,振动(正弦和随机)和热震试验。机械和环境测试已逐步进行:从单个子系统的测试到组装的Cubesat纳米卫星的测试。在所有测试活动中均已执行功能测试,以验证系统的功能。测试的顺序遵循“边走边测试”的原则,同时通过定制ESA标准ECSS-E-ST-10-03C和GEVS GSFC-STD-7000A选择持续时间和水平。

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